The effects of structural flap-lag and pitch-lag coupling on soft inplane hingeless rotor stability in hover

The effects of structural flap-lag and pitch- ...
William G. Bousman
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Last edited by WorkBot
January 20, 2010 | History

The effects of structural flap-lag and pitch-lag coupling on soft inplane hingeless rotor stability in hover

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Edition Availability
Cover of: The effects of structural flap-lag and pitch-lag coupling on soft inplane hingeless rotor stability in hover
The effects of structural flap-lag and pitch-lag coupling on soft inplane hingeless rotor stability in hover
1990, National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, For sale by the National Technical Information Service]
Microform in English

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Book Details


Edition Notes

Prepared at Ames Research Center and the Aeroflightdynamics Directorate, U.S. Army Aviation Research and Technology Activity.

Includes bibliographical references : (p. 56).

Also available via Internet from the NASA Technical Report Server web site. Address as of 12/2/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900019187%5F1990019187.pdf ; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1990]. 1 microfiche.

Published in
Washington, D.C, [Springfield, Va
Series
NASA technical paper -- 3002., AVSCOM technical report -- 89-A-002.

The Physical Object

Format
Microform
Pagination
vii, 56 p.
Number of pages
56

ID Numbers

Open Library
OL16131128M

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January 20, 2010 Edited by WorkBot add subjects and covers
December 11, 2009 Created by WorkBot add works page